HD34-24-33PN-059

Product Specification 108-151014 12Sep2018 Rev B1 HD30 Series Connector System 1. SCOPE 1.1. Content This specification covers performance, tests and quality requirements for the TE Connectivity (TE) HD30 Series Connector System. 1.2. Qualification When tests are performed on the subject product line, procedures specified in Figure 2 shall be used. All inspections shall be performed using the applicable inspection plan and product drawing. 1.3. Qualification Test Results Successful qualification testing on the subject product line was completed. The Qualification Test Report number for this testing is 501-151036_DTR-HD30. This document is on file at and available from Product Engineering, Industrial Commercial Transportation (ICT). 2. APPLICABLE DOCUMENTS AND FORMS The following documents and forms constitute a part of this specification to the extent specified herein. Unless otherwise indicated, the latest edition of the document applies. 2.1. TE Connectivity (TE) Documents • • • • • • • 0425-013-1800: 0425-014-2400: 0425-016-0000: 109-1: 114-151000: 408-151007: 501-151036: • Product Drawings Arrangement of Contact Locations for size 18 HD30 Arrangement of Contact Locations for size 24 HD30 HD30 Series Performance and Application Characteristics General Requirements for Testing Application Specification for DEUTSCH Size 16 S&F Pin & Socket Instruction Guide DEUTSCH Extraction Tools HD30 Qualification Test Report HD34-18-XXP/SX – Size 18 Receptacles HD34-24-XXP/SX – Size 24 Receptacles HD36-18-XXP/SX – Size 18 Plugs HD36-24-XXP/SX – Size 24 Plugs © 2018 TE Connectivity family of companies All Rights Reserved | Indicates Change This controlled document is subject to change. For latest revision and Regional Customer Service, visit our website at www.te.com PRODUCT INFORMATION 1-800-522-6752 *Trademark. TE Connectivity, TE connectivity (logo), and TE (logo) are trademarks. Other logos, product, and/or company names may be trademarks of their respective owners. 1 of 12 108-151014 • Product Part Numbers X refers to N, T, E seal type. XXXX refers to special modification. HD34-18-6PX-XXXX HD34-18-6SX-XXXX HD34-18-8PX-XXXX HD34-18-8SX-XXXX HD34-18-14PX-XXXX HD34-18-14SX-XXXX HD34-18-20PX-XXXX HD34-18-20SX-XXXX HD34-18-21PX-XXXX HD34-18-21SX-XXXX HD34-24-7PX-XXXX HD34-24-7SX-XXXX HD34-24-9PX-XXXX HD34-24-9SX-XXXX HD34-24-14PX-XXXX HD34-24-14SX-XXXX HD34-24-16PX-XXXX HD34-24-16SX-XXXX HD34-24-18PX-XXXX HD34-24-18SX-XXXX HD34-24-19PX-XXXX HD34-24-19SX-XXXX HD34-24-21PX-XXXX HD34-24-21SX-XXXX HD34-24-23PX-XXXX HD34-24-23SX-XXXX HD34-24-29PX-XXXX HD34-24-29SX-XXXX HD34-24-31PX-XXXX HD34-24-31SX-XXXX HD34-24-33PX-XXXX HD34-24-33SX-XXXX HD34-24-35PX-XXXX HD34-24-35SX-XXXX HD34-24-47PX-XXXX HD34-24-47SX-XXXX HD34-24-91PX-XXXX HD34-24-91SX-XXXX 12Sep2018 Rev B1 6 pin Receptacle 6 socket Receptacle 8 pin Receptacle 8 socket Receptacle 14 pin Receptacle 14 socket Receptacle 20 pin Receptacle 20 socket Receptacle 21 pin Receptacle 21 socket Receptacle 7 pin Receptacle 7 socket Receptacle 9 pin Receptacle 9 socket Receptacle 14 pin Receptacle 14 socket Receptacle 16 pin Receptacle 16 socket Receptacle 18 pin Receptacle 18 socket Receptacle 19 pin Receptacle 19 socket Receptacle 21 pin Receptacle 21 socket Receptacle 23 pin Receptacle 23 socket Receptacle 29 pin Receptacle 29 socket Receptacle 31 pin Receptacle 31 socket Receptacle 33 pin Receptacle 33 socket Receptacle 35 pin Receptacle 35 socket Receptacle 47 pin Receptacle 47 socket Receptacle 9 pin Receptacle 9 socket Receptacle HD36-18-6PX-XXXX HD36-18-6SX-XXXX HD36-18-8PX-XXXX HD36-18-8SX-XXXX HD36-18-14PX-XXXX HD36-18-14SX-XXXX HD36-18-20PX-XXXX HD36-18-20SX-XXXX HD36-18-21PX-XXXX HD36-18-21SX-XXXX HD36-24-7PX-XXXX HD36-24-7SX-XXXX HD36-24-9PX-XXXX HD36-24-9SX-XXXX HD36-24-14PX-XXXX HD36-24-14SX-XXXX HD36-24-16PX-XXXX HD36-24-16SX-XXXX HD36-24-18PX-XXXX HD36-24-18SX-XXXX HD36-24-19PX-XXXX HD36-24-19SX-XXXX HD36-24-21PX-XXXX HD36-24-21SX-XXXX HD36-24-23PX-XXXX HD36-24-23SX-XXXX HD36-24-29PX-XXXX HD36-24-29SX-XXXX HD36-24-31PX-XXXX HD36-24-31SX-XXXX HD36-24-33PX-XXXX HD36-24-33SX-XXXX HD36-24-35PX-XXXX HD36-24-35SX-XXXX HD36-24-47PX-XXXX HD36-24-47SX-XXXX HD36-24-91PX-XXXX HD36-24-91SX-XXXX 6 pin Plug 6 socket Plug 8 pin Plug 8 socket Plug 14 pin Plug 14 socket Plug 20 pin Plug 20 socket Plug 21 pin Plug 21 socket Plug 7 pin Plug 7 socket Plug 9 pin Plug 9 socket Plug 14 pin Plug 14 socket Plug 16 pin Plug 16 socket Plug 18 pin Plug 18 socket Plug 19 pin Plug 19 socket Plug 21 pin Plug 21 socket Plug 23 pin Plug 23 socket Plug 29 pin Plug 29 socket Plug 31 pin Plug 31 socket Plug 33 pin Plug 33 socket Plug 35 pin Plug 35 socket Plug 47 pin Plug 47 socket Plug 9 pin Plug 9 socket Plug 2 of 12 108-151014 2.2. Industry Documents • • • • • • • DIN 40050-9: Road Vehicles Degrees of Protection (IP Code) DIN 72551-6: Road Vehicles—Low-Tension Cables—Part 6: Single-Core, Unscreened with Thin Insulation Wall; Dimensions, Materials, Marking EIA-364: Electrical Connector/Socket Test Procedures Including Environmental Classifications IEC-60512: Electronic Equipment - Tests and Measurements IEC-60529: Degrees of Protection Provided by Enclosures (IP Code) ISO 6722: Road Vehicles—60 V and 600 V Single-Core Cables—Dimensions, Test Methods and Requirements SAE J1128: Low Voltage Primary Cable 3. REQUIREMENTS 3.1. Design and Construction Product shall be of the design, construction, materials and physical dimensions specified on the applicable product drawing. 3.2. Ratings • • Voltage: 250 V AC/DC, except 24-29, 24-31, 24-47 arrangements are 200 V AC/DC Current (Amp): See Figure 1 Contact Wire Size All Circuits Size AWG [mm²] Energized (A) 4 8 4 [25.0-21.0] 6 [16.0-13.0] 8 [10.0-8.0] 60 10 [6.0-5.0] 40 10 [6.0-5.0] 12 100 12 [4.0-2.5] 14 [2.0] 25 18 12 [2.5] 14 [2.0] 16 13 16 [1.5-1.0] 18 [0.8-0.75] 10 20 [0.5] 7.5 16 [1.5-1.0] 20 18 [0.8-0.75] 7.5 20 [0.5] 22 [0.35] 5 Figure 1 • • • Temperature: -55°C to +125°C Ingress Protection (IP) Level: IP67 Flammability: Not Applicable 12Sep2018 Rev B1 3 of 12 108-151014 3.3. Test Requirements and Procedures Summary Unless otherwise specified, all tests shall be performed at ambient environmental conditions. See Appendix A for additional test requirements See Appendix B for Test Procedure Comparison Chart Test Description Examination of Product Requirement The connectors shall be correctly constructed, marked and shall show good quality and workmanship Procedure EIA-364-18. Visually inspected for use of materials, proper construction, correct part number and insert markings and over-all quality of workmanship. Poor molding fabrication, loose materials, damaged or improperly manufactured contacts, galling of metal parts, nicks and burrs of metal parts, torn seals or cracked plastic were considered adequate basis for rejection. ELECTRICAL Insulation Resistance 1000 MΩ minimum at 25°C MIL-STD-1344, Method 3003.1 Using a 500 VDC megaohmmeter check each contact to all other contacts and the shell electrically connected together. Dielectric Withstanding Voltage No evidence of breakdown or flashover or current leakage in excess of 2.0 milliamps. Contact Resistance Maximum voltage drop across a 6 inch wire/contact assembly shall be 77 mV max for 12AWG and 89mV max for 16AWG Calculated resistance across mated contact pair shall not exceed 6 mΩ using 100 mA current. MIL-STD-1344, Method 3001.1 Check each contact to all other contacts and the shell electrically connected together for breakdown / flashover when subjected to a 1500 VAC test potential for a period of 1 minute. MIL-STD-1344, Method 3004.1 23A for size 12 (12AWG) 13A for size 16 (16AWG) Low Level Contact Resistance MIL-STD-1344, Method 3002.1 The resistance of an equal length of wire shall be subtracted from all readings to determine the added resistance of the terminal. MECHANICAL Maintenance Aging There shall be not visible change or damage to the contact cavities Contact Retention The contact shall remain in place Durability No evidence of damage to the contacts, contacting plating, connector housing or seals detrimental to reliable connector performance. Coupling torque must not increase as a result of cycling past the point where it can reasonably be done by hand. MIL-STD-1344, Method 2002.1 Subject 10% of the cavities to 10 cycles of inserting and removing its respective contact. Insert by hand, remove using removal tool. MIL-STD-1344, Method 2007.1 Subject each wired contact to an applied load of 30 lbf (size 12) and 25 lbf (size 16) for a period of 15 seconds in a direction tending to push the contact or of the rear of the connector. MIL-STD-1344, Method 2016 The connector shall be mated and unmated for a total of 100 complete cycles at room temperature Figure 2 12Sep2018 Rev B1 4 of 12 108-151014 Test Description Requirement Procedure Tool Abuse There shall be no visible damage to the connector seals or contact cavities. Use the applicable removal tool shall be inserted into the connector. With an axial load of 5 lbf applied, the tool shall be rotated 180° and then removed, also removing the terminal. Repeat 3 times. Vibration No discontinuity in excess of 1.0 µs at 100 mA during the last hour of each axis. Shall meet visual requirements, show no physical damage and meet requirements of additional tests as needed. Shock No discontinuity in excess of 1.0 µs at 100 mA during the last hour of each axis. Shall meet visual requirements, show no physical damage and meet requirements of additional tests as needed. MIL-STD-1344, Method 2005.1 Sine Sweep: 10 to 2000 Hz Sweep Cycle: 20 minutes Initial Displacement: .07 inch DA Maximum Max Acceleration: 20G’s Test Duration: 12 hours Time Per Axis X, Y, Z: 4 hours Test Current first 3 hours each axis: 12AWG = 23A, 16AWG = 13A MIL-STD-1344, Method 2004.1 10 cycles of ½ sine pluses, 50g±15%, 11±1 ms duration X and Z axis are to be tested. ENVIRONMENTAL Temperature Life There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Meet 500 MΩ minimum. Salt Spray There should be no evidence of corrosion on the connector or terminals after the connector is removed from the test and cleaned with tap water. Standard pressure is 32.68 torr. The wire mated connectors shall be immersed in a container of tap water, placed in an altitude chamber such that the water covers the connector being tested. There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Altitude Immersion Fluid Immersion 12Sep2018 Rev B1 MIL-STD-1344, Method 1005.1 The wired mated connectors shall be subjected to 100 hours at 125°C. Insulation resistance shall be measured immediately after removing sample from oven. MIL-STD-1344, Method 1001.1 Connector shall be fully mated, then submerged in a fine mist of 5% by weight of salt solution for 96 hour. MIL-STD-1344, Method 1004.1 Chamber pressure reduced to 32.68 torr and maintained for 30 minutes, then returned to atmospheric pressure within 1 minute and maintained for another 30 minutes. Test repeated for three times. MIL-STD-1344, Method 1016 Subject each connector to one fluid only. The wired mated connectors shall be submerged in the fluids below at ambient temperature. Each connector shall be submerged for 5 minutes, then removed from the fluid to air dry for 24 hours. This cycle is to be completed a total of 5 cycles. -Motor Oil 30 weight -Brake Fluid (disc type 1) -Gasoline -Diesel Fuel #2 -Antifreeze Solution (max protection) -Gear Oil 90 weight 5 of 12 108-151014 Test Description Thermal Shock External Bending Moment Insert Retention Coupling/ Uncoupling Torque Requirement Procedure There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Meet insulation resistance 500 MΩ minimum. No discontinuity in excess of 1.0 µs at 100 mA during the test. MIL-STD-1344, Method 1003.1 Cycle mated connectors for 30 minutes at –67°F followed by 30 minutes at +257°F with 2 minute max transfer time. Repeat for 5 cycles. Insulation resistance measured during last heat cycle. Mount the Receptacle panel mounted in normal service to a rigid plane. Apply a 250 in-lbf bending moment at a rate of 1.0 lbf per second for 60 seconds MIL-STD-1344, 2010.1 Apply a pulling force of 100 lbf at a rate of 10 lbf per second to the wire bundle that exist the rear of the connector for a period of 30 seconds. The inserts shall retain their proper location inside the housing. There shall be no evidence of cracking, breaking, separation from housing or loose parts. Coupling torque for mating and unmating connectors to be MIL-STD-1344, Method 2013.1 The Receptacle connector of each sample mated pair shall be mounted on a torque testing fixture and stay stationary. . Figure 2 end 12Sep2018 Rev B1 6 of 12 108-151014 3.4. Product Qualification and Requalification Test Sequence Test Group No. (a) Test or Examination 1 2 3 4 5 6 1 2 3 1 2 3 Test Sequence (b) Examination of Product Insulation Resistance Dielectric Withstanding Voltage Maintenance Aging Temperature Life Contact Retention Durability Tool Abuse Salt Spray Altitude Immersion Fluid Immersion Thermal Shock Vibration Shock External Bending Moment Insert Retention Low Level Contact Resistance Coupling/Uncoupling Torque Contact Resistance Final Examination 1 2 3 4 1 2 3 1 2 3 4 4 5 1 2 3 4 5 5 6 6 7 8 7 8 9 9 10 11 12 5 6 7 8 9 10 11 12 13 14 10 11 12 13 4 4 5 5 6 7 6 6 7 8 9 8 10 7 11 12 8 9 10 13 14 15 9 10 NOTE (a) Specimens shall be prepared in accordance with applicable product drawings and shall be selected at random from current production. (b) All cavities use wire gauge per SAE J1128 suitable for the terminal size and with sufficient length to accommodate testing. The wire insulation shall be within the connector wire sealing range. Crimp characteristics (i.e. crimp height, crimp width, etc.) shall be checked prior to testing. (c) Specimen shall consist of 24-19 arrangement connectors with DEUTSCH Solid Terminal System size 12 and 16 nickel plated pins and sockets on 12 AWG GXL and 16 AWG GXL wire. (d) All unsealed cavities shall be secured with sealing Plugs. To prevent capillary action on the sealed connector, all free wire ends and test points (i.e. millivolt test connection) shall be sealed with alcohol-based RTV silicone or equivalent and covered with heat shrink tubing (e) Numbers indicate sequence in which tests are performed. 12Sep2018 Rev B1 7 of 12 108-151014 3.5. Appendix A Additional Test Requirements Test Description Requirement Procedure ELECTRICAL Low Level Contact Resistance EIA-364-23 Test with applied voltage not to exceed 20 mV open circuit and the test current shall be limited to 100 mA. The resistance of an equal length of wire (reference wire) shall be subtracted from the same reel as used for the connector wiring. Contact Resistance EIA-364-06 Using test currents as defined. The resistance of an equal length wire (reference wire) shall be subtracted from the actual readings to determine the added resistance of the terminal. The reference wire shall be from the same reel as used for the connector wiring. 12Sep2018 Rev B1 8 of 12 108-151014 Test Description Requirement Procedure MECHANICAL Vibration There shall be no discontinuity in excess of one (1) μs at 20mV and 100 mA during the last hour of each axis. Shall meet visual requirements, show no physical damage and meet requirements of additional tests as needed. EIA-364-28 Sine Sweep: 10 to 2000 Hz Initial Displacement: 1.78 mm DA Maximum Acceleration: 20 G’s Test Duration: 12 hours Time Per Axis X, Y, Z: 4 hours Test Current first 3 hours each axis: Impact There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Small chips and dents that do not adversely affect the connector shall be disregarded. Wired mated connector shall be dropped from a height of 1.2m on a cement floor. This action is to be completed a total of five (5) times. Connector Retention There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test Apply a pulling force to the wire bundles that exit the rear of the connector for a period of one (1) minute. The amount of load is to be 111N, times the number of cavities, up to a maximum of 445N. 12Sep2018 Rev B1 9 of 12 108-151014 Test Description Requirement Contact Retention The contact shall remain in place. Temperature Life There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Procedure EIA-364-29 Using same cavities from for maintenance aging, subject to a direct load as specified below for 15 seconds in a direction tending to push the contact out of the rear of the connector. Either a Tension Testing Machine or equivalent weights may be used. ENVIRONMENTAL EIA-364-17 The wired mated connectors shall be subjected to 1000 hours at +125°C without current flowing as per MIL-STD202, Method 108, Test Condition D. ELECTRICAL Thermal Cycle There shall be no evidence of cracking, distortion or detrimental damage to the connector following the test. Cycle mated connectors from –55°C to +125°C. Connectors to remain at each temperature extreme for one (1) hour minimum. Mated connectors are to be cycled a total of 20 complete cycles. Water Immersion Test samples must meet insulation resistance. The wired mated connectors shall be placed in an oven at +125°C for two (2) hours minimum then immediately be placed in water with a 5% salt by weight content and 0.1 g/L wetting solution to a depth of 914mm for four (4) hours minimum. The free ends of the mated connectors must remain out of the water to prevent wicking of the water through the open wires. Water temperature to be +23°C. 12Sep2018 Rev B1 10 of 12 108-151014 3.6. Appendix B Test Procedure Comparison Chart Test Examination of Product Insulation Resistance Dielectric Withstanding Voltage Low Level Contact Resistance Contact Resistance Maintenance Aging Contact Retention Durability Vibration Shock Impact Connector Retention Temperature Life Salt Spray Fluid Immersion Thermal Cycle Thermal Shock Moisture Water Immersion Altitude Immersion External Bending Moment Insert Retention Coupling/Uncoupling Torque 12Sep2018 Rev B1 MIL-STD-1344 Method 3003.1 3001.1 3002.1 3004.1 2002.1 2007.1 2016 2005.1 2004.1 1005.1 1001.1 1016 1003.1 1004.1 2010.1 2013.1 EIA-364 Dash No. 18 21 20 23 06 24 29 09 28 27 42 17 26 10 32 - Similar to SAE J2030 Paragraph 6.1 6.3 6.2 6.4 6.6 6.18 6.11 6.15 6.16 6.17 6.20 6.7 6.12 6.14 6.13 6.19 - Similar to ISO 8092-2 Paragraph 4.2 4.12 4.13 4.8 4.8 4.7 4.3 4.20 4.18 4.16 4.23 4.22 4.9 - 11 of 12 108-151014 3.7. Revision History Rev Ltr Brief Description of Change Date Dwn Apvd A Initial Release 25-Oct-2017 PV DM B General Specification clarification to reflect actual product specification, updated Figure 1 to include 4AWG and other missing wire gage specs, updated durability requirement to match actual, added missing MIL-STD-1344 test procedures as needed, Appendix A added. 22AWG to LLCR Table, updated requirement CR Table, updated vibration test current, added missing contact retention 19-Dec-2017 VNB DM B1 Page 5, Fluid Immersion row, Procedure column; Changed Transmission Oil to Gear Oil. 12-Sep-2018 DD DM 12Sep2018 Rev B1 12 of 12